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PCADGRATE
Static Version: Mean --- Full Range

One Week Three Month One Year Five Year Full Range Min Mean Max

Delta/Yr below is a slope of the linear fitting over the data of the period. Delta/Yr/Yr is a slope of the liner fitting over the devivative data of the period. Slope listed on a linked plot is the slope computed on the last few periods of the data to show the direction of the trend, and different from that of Delta/Yr.

MSID MeanRMSDelta/YrDelta/Yr/YrUnitDescriptionLimit Violation
ai1ax1xon-9.936e-044.103e-04-0.01 +/- 0.17-(1.18+/-1.90)e-4DEG/SIRU-1 AXIS 1X ANALOG RATENo Violation
off-0.0043.355e-04-3.88 +/- 0.22(8.99+/-10.50)e-4No Violation
ai1ax1yon-0.0014.121e-04-0.01 +/- 0.17-(1.30+/-15.97)e-5DEG/SIRU-1 AXIS 1Y ANALOG RATENo Violation
off-0.0043.372e-04-3.91 +/- 0.22(2.40+/-7.39)e-4No Violation
ai1ax2xon-5.230e-044.112e-04-0.01 +/- 0.17(8.69+/-28.06)e-5DEG/SIRU-1 AXIS 2X ANALOG RATENo Violation
off-0.0043.360e-04-3.89 +/- 0.22(6.46+/-9.76)e-4No Violation
ai1ax2yon-5.095e-044.131e-04-0.01 +/- 0.17(9.36+/-21.49)e-5DEG/SIRU-1 AXIS 2Y ANALOG RATENo Violation
off-0.0043.368e-04-3.91 +/- 0.22(4.39+/-7.66)e-4No Violation
ai2ax1xon0.0012.133e-04-0.01 +/- 0.14(2.04+/-1.68)e-4DEG/SIRU-2 AXIS 1X ANALOG RATENo Violation
off0.0040.003-3.72 +/- 0.21-(5.27+/-160.20)e-4No Violation
ai2ax1yon0.0012.154e-04-0.01 +/- 0.14(5.89+/-16.66)e-5DEG/SIRU-2 AXIS 1Y ANALOG RATENo Violation
off6.649e-040.003-3.72 +/- 0.21-0.00 +/- 0.02No Violation
ai2ax2xon0.0012.148e-04-0.01 +/- 0.14(1.71+/-1.87)e-4DEG/SIRU-2 AXIS 2X ANALOG RATENo Violation
off0.0020.003-3.72 +/- 0.21-0.00 +/- 0.01No Violation
ai2ax2yon0.0012.153e-04-0.01 +/- 0.14(6.57+/-12.36)e-5DEG/SIRU-2 AXIS 2Y ANALOG RATENo Violation
off9.068e-040.003-3.72 +/- 0.21-0.00 +/- 0.02No Violation
aoalpang -0.3930.016-13.10 +/- 13.840.38 +/- 0.38DEGFSS ALPHA ANGLE MEASNo Violation
aoattqt1 -9.953e-044.430e-040.02 +/- 0.37-0.01 +/- 0.01naESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI)No Violation
aoattqt2 -0.0024.931e-04-0.03 +/- 0.41(6.38+/-94.08)e-4naESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI)No Violation
aoattqt3 5.715e-054.425e-04-0.04 +/- 0.370.00 +/- 0.01naESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI)No Violation
aoattqt4 -1.955e-042.263e-040.42 +/- 0.190.00 +/- 0.01naESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI)No Violation
aobetang -0.1700.025-17.20 +/- 20.69-0.23 +/- 0.55DEGFSS BETA ANGLE MEASNo Violation
aocmdqt1 -394.354609.526(5.01+/-503.40)e3-0.00 +/- 0.01naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 1No Violation
aocmdqt2 -0.0024.930e-04-0.03 +/- 0.410.00 +/- 0.01naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 2No Violation
aocmdqt3 -679.677380.024(3.02+/-313.90)e3-0.00 +/- 0.01naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 3No Violation
aoscpos1 1.347e+0334.712(1.35+/-30.61)e333.01 +/- 190.92KMSPACECRAFT POSITION VECTOR X (ECI FRAME)No Violation
aoscpos2 -1.277e+0360.560-(3.97+/-5.10)e4-(7.51+/-2.90)e2KMSPACECRAFT POSITION VECTOR Y (ECI FRAME)No Violation
aoscpos3 600.65241.240(6.76+/-3.44)e4(2.41+/-2.36)e2KMSPACECRAFT POSITION VECTOR Z (ECI FRAME)No Violation
aoscvel1 5.742e-057.337e-04-(6.60+/-6060.00)e-40.01 +/- 0.01KMPSSPACECRAFT VELOCITY VECTOR X ECI FRAME)No Violation
aoscvel2 0.0010.0010.01 +/- 0.90-0.01 +/- 0.01KMPSSPACECRAFT VELOCITY VECTOR Y (ECI FRAME)No Violation
aoscvel3 -7.610e-040.001-0.01 +/- 0.890.01 +/- 0.01KMPSSPACECRAFT VELOCITY VECTOR Z (ECI FRAME)No Violation
aosunec1 0.0028.579e-04-0.00 +/- 0.71-(3.58+/-75.77)e-4naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME)No Violation
aosunec2 -4.800e-047.829e-040.01 +/- 0.650.01 +/- 0.01naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME)No Violation
aosunec3 -2.137e-043.396e-040.00 +/- 0.280.00 +/- 0.00naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME)No Violation
aosunsa1 -2.411e-041.052e-05-0.00 +/- 0.01-(7.95+/-14.57)e-5naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME XNo Violation
aosunsa2 2.723e-042.184e-050.00 +/- 0.02-(1.66+/-4.91)e-4naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME YNo Violation
aosunsa3 3.565e-066.253e-06-1.00 +/- 0.01(3.66+/-3.37)e-5naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME ZNo Violation
aotarqt1 -9.106e-044.418e-040.02 +/- 0.36-0.01 +/- 0.01naTARGET ATTITUDE QUATERNION ELEMENT 1No Violation
aotarqt2 -0.0024.918e-04-0.03 +/- 0.41(7.19+/-93.85)e-4naTARGET ATTITUDE QUATERNION ELEMENT 2No Violation
aotarqt3 7.532e-054.418e-04-0.04 +/- 0.36-(2.30+/-111.10)e-4naTARGET ATTITUDE QUATERNION ELEMENT 3No Violation

If you have any questions, please contact swolk@cfa.harvard.edu.

Data Updated: Apr 18, 2026
Last Site Modification: Sep 30, 2021